As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENGINE INLET COWL LEADING EDGE PREVIOUS REPAIR AT BS 1089 WL 314 AT 9 O'CLOCK POSITION DOES NOT CONFORM TO AERODYNAMIC SMOOTHNESS REQUIRED FOR CRITICAL AREAS. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER IAW SRM 54-30-3 FIGURE 3. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED IAW SRM 54-30-3 FIGURE 2 AND 51-30-2.